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Jets, Wakes and Cavities. G. Birkhoff and E. H. Zarantonello. Applied Mathematics and Mechanics: Volume Two. Academic Press, New York. Academic Books, London, 1957. 353 pp. Illustrated. $10.00.
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- The Aeronautical Journal / Volume 61 / Issue 563 / November 1957
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- 28 July 2016, p. 784
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Lectures on Partial Differential Equations. I. G. Petrovsky. Translated from the Russian by A. Shenitzer. Interscience Publishers, New York, 1954. 245 pp. 41s.
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- The Aeronautical Journal / Volume 59 / Issue 536 / August 1955
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- 28 July 2016, p. 575
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A Two-Parameter Method for Calculating the Two-Dimensional Incompressible Laminar Boundary Layer
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- The Aeronautical Journal / Volume 71 / Issue 674 / February 1967
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- 04 July 2016, pp. 117-123
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The Theory of Jets in an Ideal Fluid.M. I. Gurevich. Pergamon Press Ltd, Oxford. 1966. Illustrations. 412 pp. £5.
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- The Aeronautical Journal / Volume 71 / Issue 681 / September 1967
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- 04 July 2016, pp. 663-664
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An Introduction to the Method of Characteristics.M. B. Abbott. Thames and Hudson, London. 1966. 243 pp. Diagrams. 84s.
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- The Aeronautical Journal / Volume 71 / Issue 673 / January 1967
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- 04 July 2016, p. 57
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Integral Transforms in Applied Mathematics J. W. Miles Cambridge University Press, 1971. 98 pp. £2.20.
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- The Aeronautical Journal / Volume 76 / Issue 735 / March 1972
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- 04 July 2016, p. 177
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The Generation of Sound by Aerodynamic Means
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- The Aeronautical Journal / Volume 65 / Issue 611 / November 1961
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- 04 July 2016, pp. 724-728
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New Methods in Laminar Boundary-Layer Theory.D. Meksyn. Pergamon, Oxford, 1961. 294 pp. Diagrams. 70s
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- The Aeronautical Journal / Volume 65 / Issue 609 / September 1961
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- 04 July 2016, p. 641
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Development and separation of a compressible laminar boundary layer under the action of a very sharp adverse pressure gradiant
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- Journal of Fluid Mechanics / Volume 84 / Issue 2 / 30 January 1978
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- 12 April 2006, pp. 385-400
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Experimental and theoretical studies of dissolution roughness
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- Journal of Fluid Mechanics / Volume 65 / Issue 4 / 2 October 1974
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- 29 March 2006, pp. 735-751
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Systematics of fullerenes and related clusters
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- The Fullerenes
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- 03 February 2010
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- 09 September 1993, pp 39-52
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2D Image Sensing Arrays with NIP Diodes
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- MRS Online Proceedings Library Archive / Volume 297 / 1993
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- 01 January 1993, 939
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- 1993
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Effects of a sharp pressure rise on a compressible laminar boundary layer, when the Prandtl number is σ = 0.72*
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- Proceedings of the Royal Society of Edinburgh. Section A: Mathematics / Volume 84 / Issue 1-2 / 1979
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- 14 November 2011, pp. 153-171
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- 1979
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An Accurate Calculation Method for Two-dimensional Incompressible Laminar Boundary Layers, Including Cases with Regions of Sharp Pressure Gradient
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- The Aeronautical Quarterly / Volume 28 / Issue 3 / August 1977
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- 07 June 2016, pp. 149-162
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- August 1977
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9.—Development and Separation of a Laminar Boundary Layer, under the Action of a Very Sharp Constant Adverse Pressure Gradient*
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- Proceedings of the Royal Society of Edinburgh. Section A: Mathematics / Volume 74 / 1976
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- 14 February 2012, pp. 119-134
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- 1976
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Development of a laminar boundary layer under conditions of continuous incipient separation*
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- Proceedings of the Royal Society of Edinburgh. Section A: Mathematics / Volume 76 / Issue 1 / 1976
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- 14 February 2012, pp. 55-66
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- 1976
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Shock-Induced Separation of a Laminar Boundary Layer in Supersonic Flow Past a Convex Corner
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- The Aeronautical Quarterly / Volume 16 / Issue 1 / February 1965
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- 07 June 2016, pp. 33-41
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- February 1965
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Heat Transfer Through a Compressible Laminar Boundary Layer
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- The Aeronautical Quarterly / Volume 13 / Issue 3 / August 1962
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- 07 June 2016, pp. 255-270
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- August 1962
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The Effects of Heat Transfer on Laminar-Boundary-Layer Separation in Supersonic Flow
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- The Aeronautical Quarterly / Volume 12 / Issue 4 / November 1961
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- 07 June 2016, pp. 309-336
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- November 1961
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The Estimation of Laminar Skin Friction, including the Effects of Distributed Suction
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- The Aeronautical Quarterly / Volume 11 / Issue 1 / February 1960
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- 07 June 2016, pp. 1-21
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- February 1960
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